WEKO3
アイテム
Effect of Solute Mixing in the Liquid Propellant of a Pulsed Plasma Thruster
http://hdl.handle.net/2261/3800
http://hdl.handle.net/2261/38000a76394d-08e5-4bf1-8626-669c7348527e
| 名前 / ファイル | ライセンス | アクション |
|---|---|---|
Koizumi_Vacuum_Original.pdf (298.7 kB)
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| Item type | 学術雑誌論文 / Journal Article(1) | |||||
|---|---|---|---|---|---|---|
| 公開日 | 2006-11-30 | |||||
| タイトル | ||||||
| タイトル | Effect of Solute Mixing in the Liquid Propellant of a Pulsed Plasma Thruster | |||||
| 言語 | ||||||
| 言語 | eng | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Electric propulsion | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Pulsed plasma thruster | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Liquid propellant | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Solute mixing | |||||
| キーワード | ||||||
| 主題Scheme | Other | |||||
| 主題 | Seeding | |||||
| 資源タイプ | ||||||
| 資源 | http://purl.org/coar/resource_type/c_6501 | |||||
| タイプ | journal article | |||||
| 著者 |
Koizumi, Hiroyuki
× Koizumi, Hiroyuki× Kawazoe, Yoko× Komurasaki, Kimiya× Arakawa, Yoshihiro |
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| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 147 | |||||
| 姓名 | 小泉, 宏之 | |||||
| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 148 | |||||
| 姓名 | 小紫, 公也 | |||||
| 著者別名 | ||||||
| 識別子Scheme | WEKO | |||||
| 識別子 | 149 | |||||
| 姓名 | 荒川, 義博 | |||||
| 抄録 | ||||||
| 内容記述タイプ | Abstract | |||||
| 内容記述 | Sodium chloride or ammonia was dissolved in the water propellant of pulsed plasma thrusters to improve the performance. Pulsed plasma thrusters using liquid propellant utilize water as attractive alternative instead of Teflon. Water propellant enables the controlling propellant mass flow and leads high specific impulse. However, liquid propellant pulsed plasma thrusters have larger plasma resistance and lower thrust power ratio than common Teflon propellant thruster. Here, sodium chloride and ammonia solution of water was examined to decrease that plasma resistance. As a result, emission lines attributed from the solute were observed using sodium chloride aqueous solution propellant, and a 5 % reduction of the plasma resistance was shown, and the thrust to power was increased. However, ammonia aqueous solution decreased the thruster performance. | |||||
| 書誌情報 |
Vacuum 巻 80, p. 1234-1238, 発行日 2006-09 |
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| ISSN | ||||||
| 収録物識別子タイプ | ISSN | |||||
| 収録物識別子 | 0042207X | |||||
| 書誌レコードID | ||||||
| 収録物識別子タイプ | NCID | |||||
| 収録物識別子 | AA00879589 | |||||
| DOI | ||||||
| 識別子タイプ | DOI | |||||
| 関連識別子 | info:doi/10.1016/j.vacuum.2006.01.042 | |||||
| フォーマット | ||||||
| 内容記述タイプ | Other | |||||
| 内容記述 | application/pdf | |||||
| 著者版フラグ | ||||||
| 値 | author | |||||
| 出版者 | ||||||
| 出版者 | Elsevier | |||||
| 関係URI | ||||||
| 識別子タイプ | URI | |||||
| 関連識別子 | http://www.elsevier.com/wps/find/journaldescription.cws_home/357/description | |||||
